The invention relates to a fusion structure of a special-shaped aircraft cabin and an engine structure, and belongs to the technical field of aircraft structures, the fusion structure of the special-shaped aircraft cabin and the engine structure comprises a cabin assembly, and the cabin assembly comprises a first cabin, a second cabin and a third cabin which are connected in sequence; the second cabin body comprises a first shell, a second shell, a third shell and a fourth shell which are in lap joint with one another, the engine is arranged in the second cabin body, the first cabin body is connected with a front skirt of the engine, and the third cabin body is connected with a rear skirt of the engine; the front skirt of the engine is connected with the first cabin body, the rear skirt of the engine is connected with the third cabin body, the front skirt of the engine is connected with the axial L-shaped end frame of the first cabin body, the rear skirt of the engine is connected with the axial L-shaped end frame of the third cabin body, and the shell of the engine is a main bearing structure of the aircraft. The shell of the engine is used for bearing main loads such as bending moment and axial force of the aircraft, and structural fusion of the engine and the cabin assembly is achieved.

    本申请涉及一种异形飞行器舱体与发动机结构融合结构,属于飞行器结构技术领域,异形飞行器舱体与发动机结构融合结构,包括舱体总装,舱体总装包括依次连接的第一舱体、第二舱体和第三舱体,第二舱体包括相互搭接的第一壳体、第二壳体、第三壳体和第四壳体,发动机,发动机设置于第二舱体内,第一舱体与发动机的前裙连接,第三舱体与发动机的后裙连接;本申请可以通过发动机的前裙与第一舱体连接,发动机的后裙与第三舱体连接,发动机的前裙与第一舱体轴向L型端框连接,发动机的后裙与第三舱体轴向L型端框连接,发动机的壳体是飞行器的主承载结构,利用发动机的壳体承受飞行器的弯矩、轴力等主要载荷,实现发动机与舱体总装的结构融合。


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    Titel :

    Fusion structure of special-shaped aircraft cabin and engine structure


    Weitere Titelangaben:

    一种异形飞行器舱体与发动机结构融合结构


    Beteiligte:
    LIU QING (Autor:in) / WANG HUI (Autor:in) / ZHANG ZHENGYI (Autor:in) / ZHU XUAN (Autor:in) / WANG WENLONG (Autor:in)

    Erscheinungsdatum :

    06.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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